CN201544001U - Welding fixture for aviation plug - Google Patents
Welding fixture for aviation plug Download PDFInfo
- Publication number
- CN201544001U CN201544001U CN 200920180014 CN200920180014U CN201544001U CN 201544001 U CN201544001 U CN 201544001U CN 200920180014 CN200920180014 CN 200920180014 CN 200920180014 U CN200920180014 U CN 200920180014U CN 201544001 U CN201544001 U CN 201544001U
- Authority
- CN
- China
- Prior art keywords
- clamp body
- fixed head
- aviation plug
- weld jig
- fixture
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
Abstract
The utility model discloses a welding fixture for an aviation plug. The welding fixture comprises a fixture body (1) with a hollow columnar structure, a fixing board (2), and a bracket (3), wherein the fixture body (1) has an open end, and the other end is fixedly mounted on the fixing board (2); the bracket (3) is mounted on one side of the fixing board (2) opposite to the fixture body (1); a cabinet panel hole (4) is formed on the bracket (2); three fixing screws (5) are arranged at one end of the fixture body (1) away from the fixing board (2) and are uniformly distributed on the circumference of the fixture body (1). When in use, the aviation plug with the special structure can be welded conveniently only by placing a CXCH aviation plug and a socket in the fixture, fixing the aviation plug and the socket by the fixing screws, and fixing the welding fixture on the cabinet through the cabinet panel hole. Accordingly, the welding fixture can achieve one-man operation so as to improve the work efficiency.
Description
Technical field
The utility model relates to a kind of weld jig, especially relates to the anchor clamps that a kind of aviation plug uses when welding.
Background technology
Along with development of electronic technology, the application of aviation plug in electronic equipment also more and more widely.Aviation plug is the electric connector that a kind of volume is little, in light weight, reliability is high, when under original circuit assembly pattern, welding the aviation plug socket, need another people to carry out auxiliary operation, especially when the Denso rack, operating process is very inconvenient, not only waste manpower, and reduced operator's operating efficiency.
The utility model content
Technical problem to be solved in the utility model is to provide a kind of aviation plug weld jig at problems of the prior art, its objective is and solve welding difficulty, an inefficient difficult problem that occurs in the aviation plug socket welding operation process, realize the one man operation, increase work efficiency.
The technical solution of the utility model is that this a kind of aviation plug comprises clamp body with weld jig, described clamp body is the column structure of hollow, one end opens wide, the other end is fixedly mounted on the fixed head, a side concrete relative with geometrical clamp on the fixed head is equipped with support, support is provided with the cabinet panel hole, and the end away from fixed head on the clamp body is provided with three hold-down screws, and three hold-down screws are evenly distributed on the circumference of clamp body.
An end that is connected with fixed head on the described clamp body is provided with three legs, and three legs are evenly distributed on the edge of circumference of clamp body, and plane, leg place is parallel with fixed head, links together by leg and swivel nut between clamp body and the fixed head.
The angular range that forms between the axis direction of described clamp body and the plane, fixed head place is 30 °<α<80 °.
The optimum angle that forms between the axis direction of described clamp body and the plane, fixed head place is 60 °.
A kind of aviation plug with above-mentioned special construction has the following advantages with weld jig:
1, this kind aviation plug only needs CXCH aviation plug, socket are placed in the middle of the clamp body with weld jig in use, fix its position by hold-down screw, and the weld jig assembly is fixed on the rack by the cabinet panel hole, just can weld easily, realize the one man operation, improved operating efficiency.
2, this kind aviation plug links together clamp body and fixed head by leg and swivel nut with weld jig, and by three hold-down screws welded part is fixed on the anchor clamps, makes to be connected firmly, to fix reliably, has increased the validity of welding.
3, this kind aviation plug becomes 60 ° with the weld jig clamp body with fixed head, and convenient welding is simple in structure, easy to operate.
Description of drawings
The utility model is described in further detail below in conjunction with accompanying drawing:
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the left view of structure shown in Figure 1.
Fig. 3 is the plan structure schematic diagram of structure shown in Figure 1.
In Fig. 1~3,1: clamp body; 2: fixed head; 3: support; 4: the cabinet panel hole; 5: hold-down screw; 6: leg; 7: swivel nut.
The specific embodiment
By Fig. 1-structure combination shown in Figure 3 as can be known, this kind aviation plug comprises clamp body 1 with weld jig, described clamp body 1 is the column structure of hollow, one end opens wide, the other end is fixedly mounted on the fixed head 2, and an end that is connected with fixed head 2 on the clamp body 1 is provided with on the edge of circumference that 6, three legs 6 of three legs are evenly distributed in clamp body 2, and plane, leg 6 place is parallel with fixed head 2, links together by leg 6 and swivel nut 7 between clamp body 1 and the fixed head 2; A side relative with geometrical clamp concrete 1 on the fixed head 2 is equipped with support 3, and support 3 is provided with cabinet panel hole 4, and on the fixed head 2 and inside that is positioned at clamp body 1 is provided with hold-down screw 5.
The optimum angle that forms between the axis direction of clamp body 1 and the plane, fixed head 2 place is 60 °.
The concrete course of work is: the centre that at first CXCH aviation plug, socket is placed on clamp body 1, fix its position by three equally distributed hold-down screws 5, and the weld jig assembly is fixed on the rack by cabinet panel hole 4, just can weld easily, realize the one man operation, improved operating efficiency.
Claims (4)
1. aviation plug weld jig, it is characterized in that: this weld jig comprises clamp body (1), described clamp body (1) is the column structure of hollow, one end opens wide, the other end is fixedly mounted on the fixed head (2), fixed head (2) is gone up a side relative with geometrical clamp concrete (1) support (3) is installed, support (3) is provided with cabinet panel hole (4), the end that clamp body (1) is gone up away from fixed head (2) is provided with three hold-down screws (5), and three hold-down screws (5) are evenly distributed on the circumference of clamp body (1).
2. a kind of aviation plug weld jig according to claim 1, it is characterized in that: described clamp body (1) is gone up an end that is connected with fixed head (2) and is provided with three legs (6), three legs (6) are evenly distributed on the edge of circumference of clamp body (2), and leg (6) plane, place is parallel with fixed head (2), links together by leg (6) and swivel nut (7) between clamp body (1) and the fixed head (2).
3. a kind of aviation plug weld jig according to claim 2 is characterized in that: the angular range that forms between the axis direction of described clamp body (1) and fixed head (2) plane, place is 30 °<α<80 °.
4. a kind of aviation plug weld jig according to claim 3 is characterized in that: the optimum angle that forms between the axis direction of described clamp body (1) and fixed head (2) plane, place is 60 °.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200920180014 CN201544001U (en) | 2009-10-21 | 2009-10-21 | Welding fixture for aviation plug |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200920180014 CN201544001U (en) | 2009-10-21 | 2009-10-21 | Welding fixture for aviation plug |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201544001U true CN201544001U (en) | 2010-08-11 |
Family
ID=42599160
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 200920180014 Expired - Fee Related CN201544001U (en) | 2009-10-21 | 2009-10-21 | Welding fixture for aviation plug |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN201544001U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102476253A (en) * | 2010-11-29 | 2012-05-30 | 七台河电业局 | L9 and Q9 type 2M head welding bridge |
CN104070261A (en) * | 2014-07-07 | 2014-10-01 | 广西玉柴机器股份有限公司 | Connector pin welding auxiliary fixture |
CN108279120A (en) * | 2018-01-28 | 2018-07-13 | 滨州学院 | A kind of fixture for fixed test aviation plug |
-
2009
- 2009-10-21 CN CN 200920180014 patent/CN201544001U/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102476253A (en) * | 2010-11-29 | 2012-05-30 | 七台河电业局 | L9 and Q9 type 2M head welding bridge |
CN102476253B (en) * | 2010-11-29 | 2014-09-24 | 七台河电业局 | L9 and Q9 type 2M head welding bridge |
CN104070261A (en) * | 2014-07-07 | 2014-10-01 | 广西玉柴机器股份有限公司 | Connector pin welding auxiliary fixture |
CN104070261B (en) * | 2014-07-07 | 2016-06-29 | 广西玉柴机器股份有限公司 | Connector pin welding auxiliary mould |
CN108279120A (en) * | 2018-01-28 | 2018-07-13 | 滨州学院 | A kind of fixture for fixed test aviation plug |
CN108279120B (en) * | 2018-01-28 | 2019-07-23 | 滨州学院 | A kind of fixture for fixed test aviation plug |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100811 Termination date: 20141021 |
|
EXPY | Termination of patent right or utility model |